View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 61219U 26145.58335647 +.00000000 +00000-0 -78420-4 0 00007
2 61219 53.1602 325.4469 0001308 82.0886 105.7378 15.31707255 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001308 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 325.4469° |
| argument of perigee: | 82.0886° |
| revolutions per day: | 15.31707255 |
| mean anomaly at epoch: | 105.7378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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